WEARING METALS AND THEIR RESPECTIVE PARTS IN DIESEL LOCOMOTIVE

INTRODUCTION

Lube oil analysis of Diesel locomotive by using several  analytical techniques for the condition monitoring and monetizing the engine is very important for the long life of the engine. The analytical techniques involves techniques such as elemental analysis by RDE-AES or ICP-AES , Fourier transform infrared spectroscopy, Viscosity measurement , Particle counting wear debris analysis and Karl Fischer moisture. However we had discussed about some of the above analytical techniques in earlier posts and rest of the techniques we will discuss in upcoming post. In this post we are going to discuss about the wear metals and their respective affected parts.

Elemental analysis is the most basic tests for the lube oil analysis, it is used to determine the presence of wear metals in diesel oil locomotives. There are two types of instruments which are generally used for the elemental analysis of lube oils , "RDE-AES & ICP-AES" ,which can detect more than 20 elements in lube oil. We will discuss in detail about the differences between both the instrument in the upcoming posts, however in the mean time they serve the same purpose of determination of wear metals in PPM level inside the lube oil .

During machinery in working , wear metal debris particles are produced by rubbing motion of mechanical component parts , are either normal wear or abnormal wear, these wearing metals can be detected using spectroscopy . The wear metals indicate their respective sources i.e engine parts. For every diesel engines certain limits are set for respective metals in ppm ,above which failure may occur because of the higher rate of wearing. So using spectroscopy it is much easier to monitor the condition and can take appropriate action before it will be too late and can save from bigger loss.

BELOW IS THE LIST OF THE WEAR METALS AND THEIR RESPECTIVE SOURCES:

WEAR METAL	SOURCES
Aluminium	Piston, inappropriate filtrations, Crankcases on Reciprocating Engines, Bearing Surfaces, Pumps, Thrust Washers.
Copper	Bushing, Thrust Plates.
Silicon	Inappropriate air filtrations.
Iron	Bushing, Shaft, Ring.
Chromium	Cylinder liner, Exhaust Valves.
Tin	Main bearing, Con rod, TSC bearing.
Lead	Con road, TSC bearing, Seals, Solder, Grease.
Sodium	Water coolant leakage into oil.
Boron	Water coolant Leakage.
Magnesium	Oil additives.
Nickel	Alloy from bearing metals.
Molybdenum	Piston rings.
Phosphorous	Anti-wear additive.
Potassium	Coolant Leak, Airborne Contaminant.
Silver	Bearing cages ( Silver Plating ).
Zinc	Anti-wear additive.
Calcium	Detergent Dispersant Additive.
Barium	Synthetic Oil Additive Synthetic Fluid.

INDUCTIVE COUPLED PLASMA OPTICAL EMISSION SPECTROMETER

INTRODUCTION

ICP/OES is one of the most powerful and popular analytical tools for the determination of trace elements in a sample types. The technique is based upon the spontaneous emission of photons from atoms and ions that have been excited in a RF discharge. Liquid and gas samples may be injected directly into the instrument, while solid samples require extraction or acid digestion so that the analytes will be present in a solution. The sample solution is converted to an aerosol and directed into the central channel of the plasma. At its core the inductively coupled plasma (ICP) sustains a temperature of approximately 10 000 K, so the aerosol is quickly vaporized. Analyte elements are liberated as free atoms in the gaseous state. Further collisional excitation within the plasma imparts additional energy to the atoms, promoting them to excited states. Sufficient energy is often available to convert the atoms to ions and subsequently promote the ions to excited states. Both the atomic and ionic excited state species may then relax to the ground state via the emission of a photon. These photons have characteristic energies that are determined by the quantized energy level structure for the atoms or ions. Thus the wavelength of the photons can be used to identify the elements from which they originated. The total number of photons is directly proportional to the concentration of the originating element in the sample.The instrumentation associated with an ICP/OES system is relatively simple. A portion of the photons emitted by the ICP is collected with a lens or a concave mirror. This focusing optic forms an image of the ICP on the entrance aperture of a wavelength selection device such as a monochromator. The particular wavelength exiting the monochromator is converted to an electrical signal by a photo detector. The signal is amplified and processed by the detector electronics, then displayed and stored by a computer.

ICP OES OPERATION 

As shown in Figure, the so-called ICP ‘‘torch’’ is usually an assembly of three concentric fused-silica tubes. These are frequently referred to as the outer, intermediate, and inner gas tubes. The diameter of the outer tube ranges from 9 to 27 mm. A water-cooled, two- or three-turn copper coil, called the load coil, surrounds the top section of the torch, and is connected to a RF generator. The outer argon flow (10–15 L min) sustains the high temperature plasma, and positions the plasma relative to the outer walls and the induction coil, preventing the walls from melting and facilitating the observation of emission signals. The plasma under these conditions has an annular shape. The sample aerosol carried by the inner argon flow (0.5–1.5 Lmin) enters the central channel of the plasma and helps to sustain the shape. The intermediate argon flow (0–1.5 Lmin) is optional and has the function of lifting the plasma slightly and diluting the inner gas flow in the presence of organic solvents.

The ICP is generated as follows. RF power, typically 700–1500 W, is applied to the load coil and an alternating current oscillates inside the coil at a rate corresponding to the frequency of the RF generator. For most ICP/OES instruments, the RF generator has a frequency of either 27 or 40 MHz. The oscillation of the current at this high frequency causes the same high-frequency oscillation of  electric and magnetic fields to be set up inside the top of the torch. With argon gas flowing through the torch, a spark from a Tesla coil is used to produce ‘‘seed’’ electrons and ions in the argon gas inside the load coil region. These ions and electrons are then accelerated by the magnetic field, and collide with other argon atoms, causing further ionization in a chain reaction manner. This process continues until a very intense, brilliant white, tear drop shaped, high-temperature plasma is formed. Adding energy to the plasma viaRF-induced collision is known as inductive coupling, and thus the plasma is called an ICP. The ICP is sustained within the torch as long as sufficient RF energy is applied in a cruder sense, the coupling of RF power to the plasma can be visualized as positively charged Ar ions in the plasma gas attempting to follow the negatively charged electrons flowing in the load coil as the flow changes direction 27 million times per second. Figure shows the temperature gradient within the ICP with respect to height above the load coil. It also gives the nomenclature for the different zones of the plasma .The induction region at the base of the plasma is ‘‘doughnut-shaped’’ as described above, and it is the region where the inductive energy transfer occurs. This is also the region of highest temperature and it is characterized by a bright continuum emission. From the IR upward towards to the tail plume, the temperature decreases. An aerosol, or very fine mist of liquid droplets, is generated from a liquid sample by the use of a nebulizer. The aerosol is carried into the center of the plasma by the argon gas flow through the induction region. Upon entering the plasma, the droplets undergo three processes. The first step is desolvation, or the removal of the solvent from the droplets, resulting in microscopic solid particulates, or a dry aerosol. The second step is vaporization, or the decomposition of the particles into gaseous state molecules. The third step is atomization, or the breaking of the gaseous molecules into atoms. These steps occur predominantly in the preheating zone . Finally, excitation and ionization of the atoms occur, followed by the emission of radiation from these excited species. These excitation and ionization processes occur predominantly in the initial radiation zone, and the normal analytical zone from which analytical emission is usually collected.

ICP OES INSTRUMENTATION

In inductively coupled plasma-optical emission spectrometry, the sample is usually transported into the instrument as a stream of liquid sample. Inside the instrument,the liquid is converted into an aerosol through a process known as nebulization. The sample aerosol is then transported to the plasma where it is desolvated, vaporized, atomized, and excited and/or ionized by the plasma. The excited atoms and ions emit their characteristic radiation which is collected by a device that sorts the radiation by wavelength. The radiation is detected and turned into electronic signals that are converted into concentration information for the analyst. A representation of the layout of a typical ICP-OES instrument is shown in Figure.

Major components and ICP-OES instrument

SAMPLE INTRODUCTION

A sample introduction system is used to transport a sample into the central channel of the ICP as either a  gas, vapor, aerosol of fine droplets, or solid particles. The general requirements for an ideal sample introduction  system include amenity to samples in all phases (solid, liquid, or gas), tolerance to complex matrices, the ability to analyse very small amount of samples (<1mL or <50 mg), excellent stability and reproducibility, high  transport efficiency, simplicity, and low cost. A wide variety of sample introduction methods have been developed, such as nebulization, hydride generation (HG), electro thermal vaporization (ETV), and laser  ablation.

• NEBULIZERS

Nebulizers are the most commonly used devices for solution sample introduction in ICP/OES. With a nebulizer, the sample liquid is converted into an aerosol and transported to the plasma. Both pneumatic and ultrasonic nebulizers (USNs) have been successfully used in ICP/OES. Pneumatic nebulizers make use of high-speed gas flows to create an aerosol, while the USN breaks liquid samples into a fine aerosol by the ultrasonic oscillations of a piezoelectric crystal. The formation of aerosol by the USN is therefore independent of the gas flow rate. Only very fine droplets (about 8 mm in diameter) in the aerosol are suitable for injection into the plasma. A spray chamber is placed between the nebulizer and the ICP torch to remove large droplets from the aerosol and to dampen pulses that may occur during nebulization. Thermally stabilized spray chambers are sometimes adopted to decrease the amount of liquid introduced into the plasma, thus providing stability especially when organic solvents are involved. Pneumatic nebulization is very inefficient, however, because only a very small fraction (less than 5%) of the aspirated sample solution actually reaches the plasma. Most of the liquid is lost down the drain in the spray chamber. However, the pneumatic nebulizer retains its popularity owing to its convenience, reasonable stability, and ease of use. Efficiency may only be a concern when sample volumes are limited, or measurements must be performed at or near the detection limit. Three types of pneumatic nebulizers are commonly employed in ICP/OES: the concentric nebulizer, the cross-flow nebulizer, and the Babington nebulizer .

 1.   CONCENTRIC NEBULIZER

The concentric nebulizer is fashioned from fused silica. Sample solution is pumped into the back end of the nebulizer by a peristaltic pump. Liquid uptake rates may be as high as 4mLmin, but lower flows are more common. The sample solution flows through the inner capillary of the nebulizer. This capillary is tapered so that flexible tubing from the pump is attached at the entrance (4mm outer diameter) and the exit has a narrow orifice approaching 100 mm or less in inner diameter. Ar gas (0.5–1.5 Lmin) is supplied at a right angle into the outer tube. This tube is also tapered so that the exit internal diameter approaches the outer diameter for the sample capillary. As the Ar passes through this narrow orifice, its velocity is greatly increased, resulting in the shearing of the sample stream into tiny droplets. Concentric nebulizers have the advantages of excellent sensitivity and stability, but the small fragile fused-silica orifices are prone to clogging, especially when aspirating samples of high salt content. Concentric nebulizers also require a fairly large volume of sample, given the high uptake rate. The microconcentric nebulizer (MCN) is designed to solve this problem. The sample uptake rate for the MCN is less than 0.1mLmin. The compact MCN employs a smaller diameter capillary (polyimide or TeflonÒ) and poly(vinylidine difluoride) body to minimize the formation of large droplets.

 2.   CROSS-FLOW NEBULIZER

A second type of pneumatic nebulizer is the cross-flow nebulizer, shown in Figure . The operation of cross-flow nebulizers is often compared to that of a perfume atomizer. Here a high speed stream of argon gas is directed perpendicular to the tip of a capillary tube (in contrast to the concentric or micro-concentric nebulizers where the high-speed gas is parallel to the capillary). The solution is either drawn up through the capillary tube by the low-pressure region created by the high-speed gas or forced up the tube with a pump. In either case, contact between the high-speed gas and the liquid stream causes the liquid to break up into an aerosol. Cross-flow nebulizers are generally not as efficient as concentric nebulizers at creating the small droplets needed for ICP analyses. However, the larger diameter liquid capillary and longer distance between liquid and gas injectors minimize clogging problems. Many analysts feel that the small penalty paid in analytical sensitivity is more than compensated for by the freedom from clogging. Another advantage of cross-flow nebulizers is that they are generally more rugged and corrosion-resistant than glass concentric nebulizers. In fact, this nebulizer is available with a Ryton body, a clear sapphire liquid capillary tip and a red ruby gas injector tip both contained in a polyetheretherketone (PEEK) body, all which provide chemical resistance to samples .

 3. BABINGTON NEBULIZER 

The third type of pneumatic nebulizer used for ICP/OES is the Babington nebulizer that allows a film of the sample solution to flow over a smooth surface having a small orifice . High-speed argon gas emanating from the hole shears the sheet of liquid into small droplets. The essential feature of this type of nebulizer is that the sample solution flows freely over a small aperture, rather than passing through a fine capillary, resulting in a high tolerance to dissolved solids In fact, even slurries can be nebulized with a Babington nebulizer. This type of nebulizer is the least susceptible to clogging and it can nebulize very viscous liquids.


SPRAY CHAMBER

Once the sample aerosol is created by the nebulizer, it must be transported to the torch so it can be injected into the plasma. Because only very small droplets in the aerosol are suitable for injection into the plasma, a spray chamber is placed between the nebulizer and the torch. Some typical ICP spray chamber designs are shown in Figure 3-10. The primary function of the spray chamber is to remove large droplets from the aerosol. A secondary purpose of the spray chamber is to smooth out pulses that occur during nebulization, often due to pumping of the solution. In general, spray chambers for the ICP are designed to allow droplets with diameters of about 10 mm or smaller to pass to the plasma. With typical nebulizers, this droplet range constitutes about 1 - 5% of the sample that is introduced to the nebulizer. The remaining 95 - 99% of the sample is drained into a waste container.

The material from which a spray chamber is constructed can be an important characteristic of a spray chamber. Spray chambers made from corrosion-resistant materials allow the analyst to introduce samples containing hydrofluoric acid which could damage glass spray chambers.


TORCH

The torches used in ICP-OES are very similar in design and function to those in the early days of ICP-OES.As shown schematically in Figure, the torches contain three concentric tubes for argon flow and aerosol injection. The spacing between the two outer tubes is kept narrow so that the gas introduced between them emerges at high velocity. This outside chamber is also designed to make the gas spiral tangentially around the chamber as it proceeds upward. One of the functions of this gas is to keep the quartz walls of the torch cool and thus this gas flow was originally called the coolant flow or plasma flow but is now called the "outer" gas flow. For argon ICPs, the outer gas flow is usually about 7 - 15 liters per minute. The chamber between the outer flow and the inner flow sends gas directly under the plasma toroid. This flow keeps the plasma discharge away from the intermediate and injector tubes and makes sample aerosol introduction into the plasma easier. In normal operation of the torch, this flow, formerly called the auxiliary flow but now the intermediate gas flow, is about 1.0 L/min. The intermediate flow is usually introduced to reduce carbon formation on the tip of the injector tube when organic samples are being analyzed. However, it may also improve performance with aqueous samples as well. With some torch and sample introduction configurations, the intermediate flow may be as high as 2 or 3 L/min or not used at all. The gas flow that carries the sample aerosol is injected into the plasma through the central tube or injector. Due to the small diameter at the end of the injector, the gas velocity is such that even the 1 L/min of argon used for nebulization can punch a hole through the plasma. Since this flow carries the sample to the plasma, it is often called the sample or nebulizer flow but in present terminology, this flow is known as the inner gas flow. Furthermore, this flow acts as the carrier gas for solid aerosols from spark ablation and laser ablation sample introduction techniques.


RADIO FREQUENCY GENERATOR  

The radio frequency (RF) generator is the device that provides the power for the generation and sustainment of the plasma discharge. This power, typically ranging from about 700 to 1500 watts, is transferred to the plasma gas through a load coil surrounding the top of the torch. The load coil, which acts as an antenna to transfer the RF power to the plasma, is usually made from copper tubing and is cooled by water or gas during operation.Most RF generators used for ICP-OES operate at a frequency between 27 and 56 MHz, most ICP generators were operated at 27.12 MHz. However, an increasing number of instruments now operate at 40.68 MHz because of improvements in coupling efficiency and reductions in background emission intensity realized at this frequency. Frequencies greater than 40 MHz also have been used but have not been as successful commercially. There are two general types of RF generators used in ICP instruments. Crystal-controlled generators use a piezoelectric quartz crystal to produce an RF oscillating signal that is amplified by the generator before it is applied at the load coil. The proper electrical parameters, such as output impedance, needed to keep the generator operating efficiently are controlled by a matching network that utilizes manual or automatic (servo mechanical) components. The speed and accuracy of this matching network are critical to the operation of this type of generator.


 DETECTION OF EMISSION

Most of the analytically useful emission lines for ICP-OES are in the 190 - 450 nm region; thus, spectrometers used for ICP-OES are usually optimized for operation in this wavelength region. However, there are also some important ICP emission lines between 160 and 190 nm and above 450 nm. Unfortunately, electromagnetic radiation in the 160 - 190 nm wavelength region is readily absorbed by oxygen molecules, and instruments must be specially designed to remove the air from the spectrometer to observe emission in this wavelength region. Removing oxygen from the spectrometer is done either by purging the spectrometer with a gas, usually nitrogen or argon, that doesn’t absorb the emission, or by removing the air from the spectrometer with a vacuum system. Recently, nitrogen filled optics maintained at atmospheric pressure and incorporating a catalyst for scrubbing the recycled nitrogen have been introduced.

1.  PMT DETECTOR

Once the proper emission line has been isolated by the spectrometer, the detector and its associated electronics are used to measure the intensity of the emission line. By far the most widely used detector for ICP-OES is the photomultiplier tube or PMT. To know more about the PMT read the topic Photomultiplier Tube.

 2. ARRAY CCD DETECTOR

Charge transfer devices  include a broad range of solid-state silicon-based array detectors. They include the charge injection device (CID) and the charge-coupled device (CCD). The CCD has found extensive use in nonspectroscopic devices such as video cameras, bar code scanners, and photocopiers. With the CTDs, photons falling on a silicon substrate produce electron–hole pairs.The positive electron holes migrate freely through the p type silicon semiconductor material, while the electrons are collected and stored temporarily by an array of metal oxide semiconductor (MOS) capacitors The CCD differs from the CID mainly in the readout scheme. The CCD is read out in a sequential charge shifting manner towards the output amplifier. The CID on the other hand may be read out in a non-destructive manner by shifting charge between adjacent electrodes, and then shifting it back again. The CID thus benefits from quick random access, even during long integration periods. Spectroscopic  applications of CTD’s has been hampered by the physical mismatch between the relatively small surface area of the detector and the large sometimes two dimensional focal plane associated with polychromators. This mismatch may be overcome, however, and one  commercial ICP spectrometer employs a CID detector having more than 250 000 pixels positioned upon an echelle focal plane. Alternative approaches have been successful with the CCD detector. In one case, a group of several CCD arrays are arranged around a Circular Optical System (CIROS) based upon a Rowland circle design. Rather than monitoring discrete wavelengths as is the case with the multiple PMT Rowland circle systems, the CIROS system provides total wavelength coverage from 120 to 800 nm, with resolution on the order of 0.009 nm

References

1. Inductively Coupled Plasma/Optical Emission Spectrometry by Xiandeng Hou and Bradley T. Jones 
2. Concepts, Instrumentation and Techniques in Inductively Coupled Plasma Optical Emission Spectrometry by Charles B. Boss and Kenneth J. Fredeen (Second edition)

CARBON MONOXIDE ANALYZER (CO ANALYZER)

INTRODUCTION

As we know that the cost of fuels are increasing day by day ,the high cost of fuels makes an economic necessity to increase the efficiency of the fuel , harness it to fullest and to minimize excess air levels and thermal air stack losses . Efforts toward combustion efficiency optimization, however, must be aimed at reducing total energy loss. This requires achieving minimum unburned combustible, as well as thermal stack losses. More precise control of air/fuel ratio, optimized for minimum total energy loss, can yield significant gains in efficiency and result in substantial savings in reduced fuel consumption.

 Flue gas concentration of carbon monoxide is a reliable and accurate indication of burner flame stoichiometry and the completeness of combustion. It is the most sensitive indicator of unburned combustibles losses. Used as a primary combustion efficiency parameter, in conjunction with oxygen analysis, carbon monoxide offers significant advantages in controlling combustion at optimum levels of excess air. Controlling air/fuel ratio to an optimum level of carbon monoxide assures minimum total energy loss, and maximum efficiency, independent of variations in burner load, fuel type and fuel quality. The measurement is relatively unaffected by air in-leakage, and burner maintenance requirements are immediately identified .

OPERATING PRINCIPLE

The CO analyser  utilizes infrared absorption spectroscopy to continuously measure CO concentration in combustion flue gases. The infrared source is mounted directly on the flue gas duct or stack on the side opposite from the receiver. Infrared energy is radiated by the source, through the flue gas, to the receiver. The receiver employs gas filter correlation and narrow band pass optical filtration with a solid state detector to determine the absorption of radiation by CO in the flue gas. These principles are illustrated in block diagram form in below given Figure . Infrared energy, radiated by the source, passes through the flue gas, where a portion of the energy is absorbed by any CO present. The remaining energy passes through the receiver window, focusing lens and, alternately, through two gas cells. One of the two cells is filled with CO,the other, nitrogen. These are inserted alternately in the optical path at a fixed frequency. Energy at the wavelengths of interest is, effectively, fully absorbed in the CO reference cell; however, energy is transmitted through the nitrogen cell without further absorption. After passing through the narrow bandpass filter, the remaining energy impinges upon the detector. Two energy levels are sensed alternately by the detector: source radiation reduced by the flue gas and reference cell CO and source radiation reduced by flue gas CO only. The resulting signals are rationed and compared with the rationed signals developed under zero CO calibration conditions. The comparative difference in ratios is used to compute flue gas CO concentration. The calibration source and span calibration cell are inserted into the optical path during automatic zero and span calibration of the instrument.

INFRARED SOURCE

The infrared source module emits broadband infrared radiation, including the waveband of interest, from 4.5 to 4.9 microns. The source consists of a stainless steel body with a conical surface for uniformity of surface temperature and maximum emissivity. The source is heated to a temperature of 1,112°F (600°C) and is controlled at this temperature to assure constant intensity. The source is fully insulated and enclosed in a carbon steel mounting sleeve designed for welding directly to the duct.

Since the IR source module is installed such that the source surface is flush with the inner wall of the duct, the source is not subject to coating or particulate buildup in most applications. Consequently, there is no purge air requirement to maintain source cleanliness. Due to the large diameter of the source surface, focusing is not required, and the source contains no focusing optics whatsoever. An added benefit of the large diameter source is insensitivity to duct vibration and elimination of the need for constant realignment otherwise required of focused systems. Maintaining the source temperature at 1,112°F (600°C) requires powering the heater at a nominal 50% duty cycle, extending the heater element life considerably. The operating life of the infrared source is approximately four

times that of conventional infrared sources

INFRARED RECEIVER MODEL

The infrared receiver module is designed to house the optics, detector and necessary electronics and hardware to determine absorption of infrared radiation emitted by the infrared source module. The infrared receiver module is designed to house the optics, detector and necessary electronics and hardware to determine absorption of infrared radiation emitted by the infrared source module.

In situ CO instrumentation employing thermoelectrically cooled, photoconductive detectors, the receiver employs a non-cooled pyro electric detector. Not only does this provide reliable, stable performance at high ambient temperature, it completely eliminates the maintenance associated with thermoelectric cooling systems.

FLUE GAS TEMPERATURE MEASUREMENT

The absorption of infrared radiation by carbon monoxide in combustion flue gases is a function of flue gas temperature. The temperature affects the density of the gas and, therefore, the number of molecules encountered by the radiation. In addition, temperature variations induce variations in the infrared absorption characteristics of carbon monoxide. To account for these variations, flue gas temperature must be measured continuously. Temperature data is input to the receiver module and communicated to the control module. The control module software is fully characterized to provide accurate temperature compensation over the full flue gas temperature range of 200°F to 600°F (93°C to 316°C).

References :

Rosemount Analytical-Product Data Sheet PDS 106510A

GLOW DISCHARGE OPTICAL EMISSION SPECTROMETRY

GDOES made its first appearance in 1968 and was designed primarily for bulk spectrochemical analysis of various metals and their alloys. Since its introduction, this method has been steadily developed and has excelled in the areas of surface and coating analysis as well. Compared with conventional excitation techniques, the striking feature of Glow Discharge Technology is the ability to discern defined surface layers of the material being examined and analyze their chemical composition. In the field of metal analysis GDOES is ideal for concentration profile analysis and surface analysis. All kinds of surface treatment processes as well as surface coating processes can be monitored by analyzing the surface and near-surface areas the treated material. Coating thickness and chemical composition can be accurately measured using the technique of depth profile analysis. GDOES is the preferred method of analysis for materials that were previously impossible to analyze by traditional methods, and it is one of the fastest methods available.


A stream of argon ions mill material from the sample surface. The sputtered material is then excited in a low pressure plasma discharge and resulting light emission is used to characterize and quantify the sample's composition. Glow Discharge offers an improved excitation source for fast, economical, accurate, and reliable sample turnaround. This source ultimately removes material from the sample surface which reduces the effects of metallurgical and chemical history inherent in all samples.
.

A Glow Discharge Optical Emission Spectrometer (GD-OES) is built of a glow discharge source and one or more optical spectrometers, including detectors, either Photomultiplier tubes or solid state detectors, usually CCD's. A schematic layout is given to the above. The spectrometer displayed here using a concave grating in the Rowland circle or Paschen-Runge configuration and photomultiplier tubes for the light detection.

The use of solid state detectors, CCD's and photo diode array's have become a common alternative to Photomultiplier tubes. These detectors allow the acquisition of the entire spectrum, or at least a large portion of it, but are usually slower than Photomultiplier tubes and therefore not suitable for very short acquisition times used in thin film analysis.

The principle of operation is fairly easy to understand. In a glow discharge, cathodic sputtering is used to remove material layer by layer from the sample surface. The atoms removed from the migrate into the plasma where they are excited through collisions with electrons or metastable carrier gas atoms. The characteristic spectrum emitted by this excited atom is measured by the spectrometer.

GDOES can be used in many industries such as :

• Automotive industry and its suppliers.
• Metalworking industry.
• Iron and steel industry.
• Aerospace industry.
• Electronics industry.
• Glass and ceramics industry.
• Surface technology.
• Galvanizing industry.
• Photovoltaic industry.
• Scientific institutes.

Advantages of GDOES

• Limited matrix effect.
• Linear working curves.
• Minimal spectral interferences.
• Excellent precision.
• Analysis of difficult materials (as-cast iron, low melting point alloys).
• Automatic cleaning between samples.
• Low reference material and gas consumption.